EP0184864A1 - Cast construction parts for internal-combustion engines incorporating reinforcing elements, and method for producing the connection between the parts and the elements - Google Patents
Cast construction parts for internal-combustion engines incorporating reinforcing elements, and method for producing the connection between the parts and the elements Download PDFInfo
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- EP0184864A1 EP0184864A1 EP85201684A EP85201684A EP0184864A1 EP 0184864 A1 EP0184864 A1 EP 0184864A1 EP 85201684 A EP85201684 A EP 85201684A EP 85201684 A EP85201684 A EP 85201684A EP 0184864 A1 EP0184864 A1 EP 0184864A1
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- cast components
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- whiskers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F7/0085—Materials for constructing engines or their parts
- F02F7/0087—Ceramic materials
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/14—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silica
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
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- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
- C04B37/021—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles in a direct manner, e.g. direct copper bonding [DCB]
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/08—Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
- C22C49/04—Light metals
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0696—W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/02—Surface coverings of combustion-gas-swept parts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
- F02F3/10—Pistons having surface coverings
- F02F3/12—Pistons having surface coverings on piston heads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2207/00—Aspects of the compositions, gradients
- B22F2207/11—Gradients other than composition gradients, e.g. size gradients
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5216—Inorganic
- C04B2235/522—Oxidic
- C04B2235/5224—Alumina or aluminates
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- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5264—Fibers characterised by the diameter of the fibers
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- C—CHEMISTRY; METALLURGY
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5276—Whiskers, spindles, needles or pins
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- C04B2235/5292—Flakes, platelets or plates
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- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
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- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/12—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on oxides
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0603—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head
- F02B2023/0612—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head the material having a high temperature and pressure resistance, e.g. ceramic
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F2001/008—Stress problems, especially related to thermal stress
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/02—Light metals
- F05C2201/021—Aluminium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0448—Steel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
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- F05C2201/046—Stainless steel or inox, e.g. 18-8
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/08—Ceramics; Oxides
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2253/00—Other material characteristics; Treatment of material
- F05C2253/16—Fibres
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
Definitions
- the invention relates to cast components which delimit the combustion chamber for internal combustion engines, such as pistons and cylinder heads, preferably consisting of light metal material, in the reinforcement bodies of which are formed by non-woven ceramic fibers or whiskers and which are subject to wear and / or high thermal stress, and a method to establish the connection between the components and the reinforcement bodies.
- the considerable increase in the specific performance as well as the service life, operational safety and economy of internal combustion engines requires that their, in particular also those components that delimit the combustion chamber, such as pistons and cylinder heads, be designed to meet the demands placed on them.
- the stress on the piston essentially consists of the mechanical load from the gas pressure and the thermal load from the high temperature level as well as stresses from the temperature gradient.
- the piston can be provided with a cold room.
- this generally does not contribute to reducing the thermal stresses, since the temperature gradient in the vicinity of the cold room is increased.
- the use of piston cooling contradicts the attempt to reduce the loss of heat from the combustion process to the coolant and the lubricating oil. On the other hand, this leads to high thermal loads on the piston crown.
- the rim edge of a piston with a combustion chamber bowl in the piston crown is subject to a particularly critical stress condition.
- the accelerated flow of the combustion gases increases the heat transfer in this zone, but the heat dissipation is hindered.
- This increases the temperature of the bowl rim and, together with the large tangential stress from the temperature distribution, leads to over-elastic stress.
- the load cools down or the internal combustion engine is switched off, residual tensile stresses develop. Since this operation occurs often occur at the bowl rim thermal fatigue cracks, which can be extended to great depth and in run at refrigerator piston in the refrigerator, which urchblasen to the D leads the combustion gases.
- the piston crown and bowl rim can be relieved by constructive optimization and reduction of the stresses from gas force and temperature distribution.
- ring carrier pistons When the risk of wear of the annular grooves so-called ring carrier pistons are used, is in which, inserted in the group consisting of an aluminum piston alloy K olben redesign in the region of at least the uppermost piston ring groove, an existing from an iron material ring carrier in the piston ring groove, is poured over an intermetallic compound layer (Technical Handbuch, Karl Schmidt GmbH, Neckarsulm 1967, pp. 106 to 107).
- the cast-in ring carrier disadvantageously increases the weight of the aluminum piston.
- Another reinforcement consists in piercing a groove in the area of the ring field of a piston made of an aluminum alloy and first spraying it out with a thin intermediate layer made of molybdenum, titanium, cobalt, nickel or their alloys as well as stainless steel using the metal spraying method, then with a stainless steel Fill steel with a high chromium content and a certain nickel content and then form the ring grooves (DE-OS 14 00 115).
- the disadvantage is that there is poor adhesive strength between the aluminum alloy and the sprayed-on intermediate layer.
- GB-PS 2 106 433 describes a light metal piston produced by pressure casting, in the bottom of which a layer of fibers or whiskers is embedded to avoid cracks.
- EP-OS 80 562 to protect against wear and / or thermal fatigue cracks in components made of light metal material, non-woven ceramic fibers with a volume fraction from 2 to 10% stored. Wear resistance and thermal insulation of such pistons or components do not meet the requirements.
- Object of the present invention is, therefore, ewehrungs stressesn cast, the combustion chamber defining components for internal combustion engines, such as pistons and cylinder heads with cast-B which have a structure formed from non-woven ceramic fibers or whiskers for surface protection against wear and / or thermal insulation To provide, which ensure long-term protection against damage to the underlying light metal material of the component in a relatively thin zone near the surface of the components.
- the fibers or whiskers have a diameter of 0.5 to 5 JU m and a diameter to length ratio of 10 to 100 and have a volume of 10 to 50%, based on the total volume of the B ewehrungs stressess occupy.
- the open pores of the stress-releasing section of the fiber or whisker structure are completely impregnated with the light metal material of the component, so that a connection between the ceramic layer formed by the hardened ceramic mass and the light metal material of the component is ensured by the fibers or whiskers, both of which Forces can be transmitted perpendicular to and in the connection plane. It is assumed that according to the prior art between the kera mix or metallic matrix and the fibers or whiskers there is a sufficiently strong bond.
- the fibers or whiskers appropriately occupy a volume of 10 to 30%, based on the total volume of the reinforcement body, and can be arranged either randomly or in such a way that they are in the claims side
- the section of the reinforcement body runs mainly parallel to the surface.
- a preferred embodiment of the invention consists in that the fiber or whisker volume fraction of the reinforcement body increases, preferably continuously, in the direction of loading, and the volume fraction of the fiber or whisker structure in the area close to the stress is> 50 vol.%, Preferably up to 70 vol.%. In special cases it is possible that this fiber or whisker structure is free of ceramic mass.
- the fiber or whisker structure is impregnated in the section on the load side to a depth of 1 to 20 mm, preferably 3 to 5 mm, with ceramic material.
- the reinforcement body can also have a cover layer made of ceramic mass on the load side.
- the transition area of the reinforcement body consisting of ceramic mass and light metal material has a layer thickness of almost zero to almost the thickness of the ceramic layer, preferably of 0.5 to 3 mm.
- the shape of the fiber or whisker structure is retained when it is poured into the component made of light metal material, it is appropriate to sinter the fibers or whiskers at their points of contact with one another or to glue them with an inorganic adhesive.
- the ceramic layer has a low open porosity, through the pores of which the air contained in the fiber or whisker structure can escape during the impregnation with the light metal material and light metal can penetrate, at least partially, into the pores in order to achieve the positive connection to reinforce.
- the liquid light metal material is cast under pressure, for example by casting presses, vacuum infiltration or the like, and the pressure or negative pressure is maintained until the light metal material solidifies.
- the reinforcement body 4 consists of a fiber structure body with irregularly arranged Al 2 O 3 fibers with an average diameter of 3 ⁇ m and a diameter-length ratio of 10 to 100.
- the fiber structure is hardened on the combustion chamber side to a depth of 3 to 5 mm Si0 2 soaked. The open pores of the fiber structure are completely filled with light metal material 5 from the opposite side.
- the structure of the cast-in reinforcement body 4 is shown in FIG. 2 in an enlarged detail from FIG.
- the hatched fiber structure 6 is impregnated in the combustion chamber section 7 with the hardened ceramic mass consisting of SiO 2 , the penetration depth of which extends irregularly into the transition region 8.
- the pores of the fiber structure 6 and the open pores of the ceramic layer are impregnated with light metal infiltrated by casting presses. This creates an excellent mechanical clamp between the ceramic layer and reached the light metal material 5.
Abstract
Bei den Brennraum begrenzenden Bauteilen aus Leichtmetall für Brennmaschinen sind in den dem Verschleiss unterliegenden Oberflächenbereichen aus ungewebten keramischen Fasern gebildete Bewehrungskörper eingegossen. Um eine Langzeit-Schutzwirkung gegenüber einer Schädigung des unter den Bewehrungskörpern liegenden Leichtmetalls zu erreichen, ist vorgesehen, die offenen Poren der Faserstruktur beanspruchungsseitig mit einer Schicht einer keramischen Masse und beanspruchungsabseitig mit dem Leichtmetall des Bauteils zu tränken.In the case of components made of light metal for internal combustion engines which delimit the combustion chamber, reinforcement bodies formed from non-woven ceramic fibers are cast into the surface areas subject to wear. In order to achieve a long-term protective effect against damage to the light metal lying under the reinforcement bodies, it is provided to impregnate the open pores of the fiber structure on the stress side with a layer of a ceramic mass and on the stress side with the light metal of the component.
Description
Die Erfindung betrifft gegossene, den Brennraum begrenzende Bauteile für Brennkraftmaschinen, wie Kolben und Zylinderköpfe, vorzugsweise aus Leichtmetallwerkstoff bestehend, in deren der Beanspruchung durch Verschleiß und/oder durch hohe thermische Belastung unterliegenden Oberflächenbereichen aus ungewebten keramischen Fasern oder Whiskern gebildete Bewehrungskörper eingegossen sind sowie ein Verfahren zur Herstellung der Verbindung zwischen den Bauteilen und den Bewehrungskörpern.The invention relates to cast components which delimit the combustion chamber for internal combustion engines, such as pistons and cylinder heads, preferably consisting of light metal material, in the reinforcement bodies of which are formed by non-woven ceramic fibers or whiskers and which are subject to wear and / or high thermal stress, and a method to establish the connection between the components and the reinforcement bodies.
Die erhebliche Steigerung sowohl der spezifischen Leistung als auch der Lebensdauer, Betriebssicherheit und Wirtschaftlichkeit von Brennkraftmaschinen erfordert eine beanspruchungsgerechte Gestaltung ihrer, insbesondere auch der den Brennraum begrenzenden Bauteile, wie Kolben und zylinderköpfe. Die Beanspruchung des Kolbens setzt sich im wesentlichen zusammen aus der mechanischen Belastung durch den Gasdruck und der thermischen Belastung durch hohes Temperaturniveau sowie Spannungen aus dem Temperaturgradienten. Um die hohe thermische Belastung zu beherrschen, kann der Kolben mit einem Kühlraum versehen werden. Dieser trägt jedoch im allgemeinen nicht zur Verminderung der Wärmespannungen bei, da der Temperaturgradient in der Umgebung des Kühlraums erhöht wird. Im übrigen widerspricht die Anwendung von Kolbenkühlung dem Bestreben, die Abgabe von Verlustwärme aus dem Verbrennungsprozeß an das Kühlmittel und das Schmieröl zu verringern. Das führt andererseits zu hoher thermischen Belastung des Kolbenbodens.The considerable increase in the specific performance as well as the service life, operational safety and economy of internal combustion engines requires that their, in particular also those components that delimit the combustion chamber, such as pistons and cylinder heads, be designed to meet the demands placed on them. The stress on the piston essentially consists of the mechanical load from the gas pressure and the thermal load from the high temperature level as well as stresses from the temperature gradient. To master the high thermal load, the piston can be provided with a cold room. However, this generally does not contribute to reducing the thermal stresses, since the temperature gradient in the vicinity of the cold room is increased. Incidentally, the use of piston cooling contradicts the attempt to reduce the loss of heat from the combustion process to the coolant and the lubricating oil. On the other hand, this leads to high thermal loads on the piston crown.
Einem besonders kritischen Beanspruchszustand unterliegt bei einem Kolben mit Brennraummulde im Kolbenboden der Muldenrand. Durch die beschleunigte Strömung der Verbrennungsgase ist der Wärmeübergang in dieser Zone verstärkt, die Wärmeableitung ist aber behindert. Dadurch steigt die Temperatur des Muldenrandes und führt zusammen mit der großen Tangentialspannung aus der Temperaturverteilung zu einer überelastischen Beanspruchung. Bei Abkühlung durch Laständerung oder Abstellen der Brennkraftmaschine bilden sich Zugeigenspannungen aus. Da dieser Vorgang häufig stattfindet, treten am Muldenrand thermische Ermüdungsrisse auf, die sich zu großer Tiefe erweitern können und bei Kühlraumkolben in den Kühlraum hineinlaufen, was zum Durchblasen der Verbrennungsgase führt.The rim edge of a piston with a combustion chamber bowl in the piston crown is subject to a particularly critical stress condition. The accelerated flow of the combustion gases increases the heat transfer in this zone, but the heat dissipation is hindered. This increases the temperature of the bowl rim and, together with the large tangential stress from the temperature distribution, leads to over-elastic stress. When the load cools down or the internal combustion engine is switched off, residual tensile stresses develop. Since this operation occurs often occur at the bowl rim thermal fatigue cracks, which can be extended to great depth and in run at refrigerator piston in the refrigerator, which urchblasen to the D leads the combustion gases.
Anfälligkeit für Verschleiß der Ringnuten am Kolben, insbesondere der obersten Ringnut, mit Bruchgefahr der Kolbenringe besteht, wenn aufgrund der konstruktiven Gesamtauslegung der Brennkraftmaschine die Temperaturen im Ringfeld abnormal hoch liegen, extreme Rückstände bildender Kraftstoff gefahren wird, aus besonderen Gründen das Spiel des Kolbens groß gewählt wurde und dadurch Kippbewegungen ermöglicht werden oder die Luftfilterung, besonders in staubreicher Umgebung, z.B. auf Baustellen, unzulänglich ist.Susceptibility to wear of the ring grooves on the piston, especially the uppermost ring groove, with risk of breakage of the piston rings, if, due to the overall design of the internal combustion engine, the temperatures in the ring field are abnormally high, extreme residue fuel is used, the piston play should be large for special reasons was and thereby tilting movements are made possible or air filtering, especially in dusty environments, e.g. on construction sites, is inadequate.
In begrenztem Umfang können Kolbenboden und Muldenrand durch konstruktive Optimierung und Abbau der Spannungen aus Gaskraft und Temperaturverteilung entlastet werden.To a limited extent, the piston crown and bowl rim can be relieved by constructive optimization and reduction of the stresses from gas force and temperature distribution.
Die Bewehrung des Muldenrandes durch einen eingegossenen nickellegierten Gußeisenring schafft für begrenzte Laufzeit Abhilfe (Fachkunde Kraftfahrtechnik, 2. Aufl., Holland + Josenhans Verlag, Stuttgart 1982, S. 27). Durch bleibende Deformation zeigt sich jedoch nach längerem Betrieb ein Spalt zwischen dem Gußeisenring und dem Kolbenboden. Weitere Nachteile dieser Bewehrung des Muldenrands bestehen in einem Anwachsen von Gewicht und Herstellungskosten des Kolbens. Anstelle des Gußeisenringes ist deshalb ein Ring aus Aluminiumtitanat vorgeschlagen worden (DE-OS 32 30 388), der jedoch nur dann eingesetzt werden kann, wenn sich dieser Ring - bedingt durch die Schrumpfverbindung - mit einer ausreichend großen Fläche gegen den ihn umgebenden Kolbenwerkstoff abstützen kann. Auf der Suche nach alternativen Lösungen, die die genannte Nachteile vermeiden, werden auch metallische und metall-keramische Flamm- und Plasmaspritzschichten auf den Kolbenbo- den aufgetragen (DE-OS 31 37 731). Der Schichtaufbau ist jedoch an den scharfen Kanten des Brennraummuldenrandes gestört. Außerdem zeigen die Schichten unzureichende Haftfestigkeiten bei besonderen Belastungsfällen. Ursächlich hierfür sind die hohen thermischen Belastungen mit der Folge allmählicher Entfestigung und Rißbildung sowie der große, entsprechend hohe Spannungen erzeugende, Temperaturgradient in der Deckschicht selbst. Schließlich ist auch bekannt (DE-OS 25 07 899), Kolbenböden mit einer 30 bis 80 jum dicken Harteloxalschicht zu überziehen, wodurch sich zwar eine deutlich verbesserte Schutzwirkung gegenüber thermischer Ermüdung ergibt, jedoch keine nennenswerte Temperatursenkung erreicht wird. Hinzuweisen ist noch auf einen Kolben (Diesel Progress North America April 1984) mit einer aus Stahlblech bestehenden Abdeckung mit einem beanspruchungsabseitig aufgesinterten Stahldrahtgewebe. Die Abdeckung wird mit dem Kolben im Gießpreßverfahren zusammengegossen. Dieser Kolben besitzt nur begrenzte Wärmedämmung und ein durch die Abdeckung und das Stahldrahtgewebe erhöhtes Gewicht.The reinforcement of the bowl rim by a cast nickel alloy cast iron ring provides for limited term remedy (expertise Automotive Technology, 2. A ufl., Holland + Jose Hans Verlag, Stuttgart 1982, p 27). Permanent deformation shows a gap between the cast iron ring and the piston crown after prolonged operation. Further disadvantages of this reinforcement of the bowl rim are an increase in the weight and manufacturing costs of the piston. Instead of the cast iron ring, a ring made of aluminum titanate has therefore been proposed (D E -O S 32 30 388), which, however, can only be used if this ring - due to the shrink connection - has a sufficiently large area against the piston material surrounding it can support. In the search for alternative solutions which avoid the disadvantages mentioned, can also be metallic and metal-ceramic flame and plasma spray coatings on the K olbenbo- the applied (DE-OS 31 37 731). However, the layer structure is disturbed at the sharp edges of the combustion chamber bowl edge. In addition, the layers show insufficient adhesive strength in special stress cases. The reason for this are the high thermal loads with the result of gradual softening and cracking and the large, correspondingly high stress-producing temperature gradient in the top layer itself. Finally, it is also known (DE-OS 25 07 899), piston crowns with a thickness of 30 to 80 μm To coat hard anodized layer, which results in a significantly improved protective effect against thermal fatigue, but no significant temperature reduction is achieved. It should also be pointed out to a piston (Diesel Progress N orth America April 1984) with a cover made of sheet steel with a steel wire mesh sintered away from the stress. The cover is cast together with the piston in a press-molding process. This piston has only limited thermal insulation and a weight which is increased by the cover and the steel wire mesh.
Bei der Gefahr des Verschleißes der Ringnuten werden sogenannte Ringträgerkolben eingesetzt, bei denen in den aus einer Aluminiumkolbenlegierung bestehenden Kolbenkörper im Bereich wenigstens der obersten Kolbenringnut ein aus einem Eisenwerkstoff bestehender Ringträger, in den die Kolbenringnut eingestochen ist, über eine intermetallische Verbundschicht eingegossen ist (Technisches Handbuch, Karl Schmidt GmbH, Neckarsulm 1967, S. 106 bis 107). Durch den eingegossenen Ringträger wird das Gewicht des Aluminiumkolbens in nachteiliger Weise erhöht. Eine andere Bewehrung besteht darin, bei einem aus einer Aluminiumlegierung bestehenden Kolben im Bereich des Ringfeldes eine Nut einzustechen und diese nach dem Metallspritzverfahren zunächst mit einer dünnen Zwischenschicht aus Molybdän, Titan, Kobalt, Nickel oder deren Legierungen sowie rostfreiem Stahl auszuspritzen, dann mit einem rostfreien Stahl mit hohem Chromgehalt und einem bestimmten Nickelgehalt aufzufüllen und danach die Ringnuten auszubilden (DE-OS 14 00 115). Der Nachteil besteht darin, daß zwischen der Aluminiumlegierung und der aufgespritzten Zwischenschicht eine schlechte Haftfestigkeit besteht.When the risk of wear of the annular grooves so-called ring carrier pistons are used, is in which, inserted in the group consisting of an aluminum piston alloy K olbenkörper in the region of at least the uppermost piston ring groove, an existing from an iron material ring carrier in the piston ring groove, is poured over an intermetallic compound layer (Technical Handbuch, Karl Schmidt GmbH, Neckarsulm 1967, pp. 106 to 107). The cast-in ring carrier disadvantageously increases the weight of the aluminum piston. Another reinforcement consists in piercing a groove in the area of the ring field of a piston made of an aluminum alloy and first spraying it out with a thin intermediate layer made of molybdenum, titanium, cobalt, nickel or their alloys as well as stainless steel using the metal spraying method, then with a stainless steel Fill steel with a high chromium content and a certain nickel content and then form the ring grooves (DE-OS 14 00 115). The disadvantage is that there is poor adhesive strength between the aluminum alloy and the sprayed-on intermediate layer.
In der GB-PS 2 106 433 ist ein durch Preßgießen hergestellter Leichtmetallkolben beschrieben, in dessen Boden eine Schicht aus Fasern oder Whiskern zur Vermeidung von Rissen eingebettet ist. Schließlich sind gemäß EP-OS 80 562 zum Schutz gegen Verschleiß und/oder thermische Ermüdungsrisse in Bauteilen aus Leichtmetallwerkstoff ungewebte keramische Fasern mit einem Volumenanteil von 2 bis 10 % eingelagert. Verschleißfestigkeit und Wärmedämmung solcher Kolben bzw. Bauteile entsprechen aber nicht den gestellten Anforderungen.GB-
Aufgabe der vorliegenden Erfindung ist es deshalb, gegossene, den Brennraum begrenzende Bauteile für Brennkraftmaschinen, wie Kolben und Zylinderköpfe, mit eingegossenen Bewehrungskörpern, die eine aus ungewebten, keramischen Fasern oder Whiskern gebildete Struktur besitzen, für den Oberflächenschutz gegen Verschleiß und/oder zur Wärmedämmung bereitzustellen, die in einer relativ dünnen oberflächennahen Zone der Bauteile eine Langzeit-Schutzwirkung gegenüber einer Schädigung des darunterliegenden Leichtmetallwerkstoffs des Bauteils gewährleisten.Object of the present invention is, therefore, ewehrungskörpern cast, the combustion chamber defining components for internal combustion engines, such as pistons and cylinder heads with cast-B which have a structure formed from non-woven ceramic fibers or whiskers for surface protection against wear and / or thermal insulation To provide, which ensure long-term protection against damage to the underlying light metal material of the component in a relatively thin zone near the surface of the components.
Gelöst ist diese Aufgabe dadurch, daß die offenen Poren der Faser- bzw. Whiskerstruktur im beanspruchungsseitigen Abschnitt mit einer Schicht einer eine geringe Porosität aufweisenden gehärteten keramischen Masse, im beanspruchungsabseitigen Abschnitt mit einer Schicht des Leichtmetallwerkstoffs und im Ubergangsbereich mit einer Schicht aus keramischer Masse und Leichtmetallwerkstoff ausgefüllt sind, die Fasern bzw. Whisker einen Durchmesser von 0,5 bis 5JUm und ein Durchmesser-Längen-Verhältnis von 10 bis 100 haben und ein Volumen von 10 bis 50 %, bezogen auf das Gesamtvolumen des Bewehrungskörpers, einnehmen.This object is achieved in that the open pores of the fiber or whisker structure in the stress-side section with a layer of a low porosity hardened ceramic mass, in the stress-away section with a layer of the light metal material and in the transition area with a layer of ceramic mass and light metal material are filled, the fibers or whiskers have a diameter of 0.5 to 5 JU m and a diameter to length ratio of 10 to 100 and have a volume of 10 to 50%, based on the total volume of the B ewehrungskörpers occupy.
Die offenen Poren des beanspruchungsabseitigen Abschnitts der Faser- bzw. Whiskerstruktur sind vollständig mit dem Leichtmetallwerkstoff des Bauteils getränkt, so daß eine Verbindung zwischen der durch die gehärtete keramische Masse gebildeten Keramikschicht und dem Leichtmetallwerkstoff des Bauteils durch die Fasern bzw. Whisker gewährleistet ist, die sowohl Kräfte senkrecht zur als auch in der Verbindungsebene übertragen kann. Dabei ist vorausgesetzt, daß nach dem Stand der Technik zwischen der keramischen bzw. metallischen Matrix und den Fasern bzw. Whiskern eine ausreichend feste Bindung besteht. Eine zusätzliche Verbindung wird an der vergleichsweise großen Grenzfläche zwischen faser- bzw. whiskerverstärkter keramischer Masse und faser- bzw. verstärktem Leichtmetallwerkstoff des Bauteils dadurch erzielt, daß der Leichtmetallwerkstoff des Bauteils in die offenen Poren der faser- bzw. whiskerverstärkten Keramikschicht so tief eindringt, daß ergänzend zu den atomaren Bindungskräften an den Grenzflächen die durch die unregelmäßige Form der Poren bedingte mechanische Verklammerung eine Erhöhung der Haftfestigkeit schafft. Durch die Faser- bzw. Whiskerstruktur im Abschnitt der Keramikschicht wird eine deutliche Verbesserung der Haftfestigkeit der Keramikschicht für den Fall erreicht, daß diese als Folge von Überbelastungen, beispielsweise durch zu große Wärmespannungen, rissig werden sollte. Die Fasern bzw. Whisker verhindern oder verzögern zumindest aufgrund ihrer gegenüber der Keramikschicht höheren Festigkeit die Rißausbreitung. Selbst wenn die Risse durch die Keramikschicht durchlaufen sollten, besteht keine Gefahr, daß sich Stücke der Keramikschicht lösen, da ja jedes Stück über Fasern bzw. Whisker und über den in die offenen Poren eingreifenden Leichtmetallwerkstoff des Bauteils fest mit dem gegossenen Bauteil verbunden ist. Ein weiterer Vorteil ist darin zu sehen, daß die Fasern bzw. Whisker eine Angleichung der thermischen Längenausdehnungskoeffizienten von keramischer Masse und Leichtmetallwerkstoff bewirken und somit die mit dem Betrieb zwangsläufig verbundenen Temperaturänderungen zu deutlich geringeren Spannungen in der Verbindungszone der Werkstoffe führen.The open pores of the stress-releasing section of the fiber or whisker structure are completely impregnated with the light metal material of the component, so that a connection between the ceramic layer formed by the hardened ceramic mass and the light metal material of the component is ensured by the fibers or whiskers, both of which Forces can be transmitted perpendicular to and in the connection plane. It is assumed that according to the prior art between the kera mix or metallic matrix and the fibers or whiskers there is a sufficiently strong bond. An additional connection is achieved at the comparatively large interface between fiber or whisker reinforced ceramic mass and fiber or reinforced light metal material of the component in that the light metal material of the component penetrates so deeply into the open pores of the fiber or whisker reinforced ceramic layer that In addition to the atomic binding forces at the interfaces, the mechanical interlocking caused by the irregular shape of the pores increases the adhesive strength. The fiber or whisker structure in the section of the ceramic layer significantly improves the adhesive strength of the ceramic layer in the event that it should crack as a result of overloading, for example due to excessive thermal stresses. The fibers or whiskers prevent or delay crack propagation, at least because of their higher strength than the ceramic layer. Even if the cracks pass through the ceramic layer, there is no danger of pieces of the ceramic layer becoming detached, since each piece is firmly connected to the cast component via fibers or whiskers and the light metal material of the component engaging in the open pores. Another advantage can be seen in the fact that the fibers or whiskers bring about an equalization of the thermal expansion coefficients of ceramic mass and light metal material and thus the temperature changes inevitably associated with operation lead to significantly lower stresses in the connecting zone of the materials.
Die Fasern bzw. Whisker nehmen zweckmäßigerweise ein Volumen von 10 bis 30 %, bezogen auf das Gesamtvolumen der Bewehrungskörper, ein und können sowohl regellos als auch in der Weise angeordnet sein, daß sie im beanspruchungsseitigen Abschnitt der Bewehrungskörper überwiegend parallel zur Oberfläche verlaufen.The fibers or whiskers appropriately occupy a volume of 10 to 30%, based on the total volume of the reinforcement body, and can be arranged either randomly or in such a way that they are in the claims side The section of the reinforcement body runs mainly parallel to the surface.
Eine vorzugsweise Ausgestaltung der Erfindung besteht darin, daß der Faser- bzw. Whiskervolumenanteil des Bewehrungskörpers in Belastungsrichtung, vorzugsweise kontinuierlich, zunimmt und der Volumenanteil der Faser- bzw. Whiskerstruktur im beanspruchungsnahen Bereich > 50 Vol.%, vorzugsweise bis 70 Vol.% ist. In besonderen Fällen ist es möglich, daß diese Faser- bzw. Whiskerstruktur frei von keramischer Masse ist.A preferred embodiment of the invention consists in that the fiber or whisker volume fraction of the reinforcement body increases, preferably continuously, in the direction of loading, and the volume fraction of the fiber or whisker structure in the area close to the stress is> 50 vol.%, Preferably up to 70 vol.%. In special cases it is possible that this fiber or whisker structure is free of ceramic mass.
Die Faser- bzw. Whiskerstruktur ist im beanspruchungsseitigen Abschnitt auf eine Tiefe von 1 bis 20 mm, vorzugsweise 3 bis 5 mm mit keramischer Masse getränkt.The fiber or whisker structure is impregnated in the section on the load side to a depth of 1 to 20 mm, preferably 3 to 5 mm, with ceramic material.
Der Bewehrungskörper kann beanspruchungsseitig noch eine Deckschicht aus keramischer Masse aufweisen.The reinforcement body can also have a cover layer made of ceramic mass on the load side.
Der aus keramischer Masse und Leichtmetallwerkstoff bestehende Ubergangsbereich des Bewehrungskörpers hat eine Schichtdicke von nahezu Null bis nahezu der Dicke der Keramikschicht, vorzugweise von 0,5 bis 3 mm.The transition area of the reinforcement body consisting of ceramic mass and light metal material has a layer thickness of almost zero to almost the thickness of the ceramic layer, preferably of 0.5 to 3 mm.
Damit die Form der Fasern- bzw. Whiskerstruktur beim Eingießen in das Bauteil aus Leichtmetallwerkstoff erhalten bleibt, ist es angebracht, die Fasern bzw. Whisker an ihren Berührungspunkten miteinander zu versintern oder mittels eines anorganischen Klebers zu verkleben.So that the shape of the fiber or whisker structure is retained when it is poured into the component made of light metal material, it is appropriate to sinter the fibers or whiskers at their points of contact with one another or to glue them with an inorganic adhesive.
Es ist von Vorteil, daß die Keramikschicht eine geringe offene Porosität aufweist, über deren Poren während des Tränkens mit dem Leichtmetallwerkstoff die in der Faser- bzw. Whiskerstruktur enthaltene Luft entweichen und Leichtmetall in die Poren, zumindest partiell, eindringen kann, um die formschlüssige Verbindung noch zu verstärken.It is advantageous that the ceramic layer has a low open porosity, through the pores of which the air contained in the fiber or whisker structure can escape during the impregnation with the light metal material and light metal can penetrate, at least partially, into the pores in order to achieve the positive connection to reinforce.
Um den beanspruchungsabseitigen Abschnitt der Faser- bzw. Whiskerstruktur mit dem Leichtmetallwerkstoff des Bauteils zu tränken, wird der flüssige Leichtmetallwerkstoff unter Druck, beispielsweise durch GieBpressen, Vakuuminfiltration oder dergleichen angegossen, und der Druck bzw. Unterdruck bis zur Erstarrung des Leichtmetallwerkstoffs aufrechterhalten.In order to impregnate the portion of the fiber or whisker structure away from the stress with the light metal material of the component, the liquid light metal material is cast under pressure, for example by casting presses, vacuum infiltration or the like, and the pressure or negative pressure is maintained until the light metal material solidifies.
Die Erfindung ist in der Zeichnung beispielhaft dargestellt.The invention is illustrated by way of example in the drawing.
Fig. 1 zeigt einen Teillängsschnitt durch einen Leichtmetallkolben 1 mit Brennraummulde 2 für Dieselmotoren, dessen Kolbenboden 3 und Brennraummulde 2 durch einen eingegossenen erfindungsgmäBen Bewehrungskörper 4 gebildet sind. Der Bewehrungskörper 4 besteht aus einem Faserstrukturkörper mit unregelmäßig angeordneten Al2O3-Fasern mit einem Durchmesser von im Mittel 3 µm und einem Durchmesser-Längen-Verhältnis von 10 bis 100. Die Faserstruktur ist brennraumseitig auf eine Tiefe von 3 bis 5 mm mit ausgehärtetem Si02 getränkt. Von der Gegenseite her sind die offenen Poren der Faserstruktur vollständig mit Leichtmetallwerkstoff 5 gefüllt.1 shows a partial longitudinal section through a
In Fig. 2 ist in einem vergrößerten Ausschnitt aus Fig. l der Aufbau des eingegossenen Bewehrungskörpers 4 wiedergegeben. Die schraffiert dargestellte Faserstruktur 6 ist im brennraumseitigen Abschnitt 7 mit der aus Si02 bestehenden ausgehärteten keramischen Masse getränkt, deren Eindringtiefe unregelmäßig bis in den übergangsbereich 8 hineinverläuft. Im brennraumabseitigen Abschnitt 9 sind die Poren der Faserstruktur 6 und die offenen Poren der Keramikschicht mit durch GieBpressen infiltrierten Leichtmetall getränkt. Dadurch wird eine ausgezeichnete mechanische Verklammerung zwischen der keramischen Schicht und dem Leichtmetallwerkstoff 5 erreicht. Brennraumseitig weist der Bewehrungskörper 4 eine aus der keramischen Masse bestehende Deckschicht 10 auf.The structure of the cast-in reinforcement body 4 is shown in FIG. 2 in an enlarged detail from FIG. The hatched
Claims (12)
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Application Number | Priority Date | Filing Date | Title |
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DE3444406 | 1984-12-05 | ||
DE19843444406 DE3444406A1 (en) | 1984-12-05 | 1984-12-05 | CASTED COMPONENTS FOR INTERNAL COMBUSTION ENGINES WITH PEGED-IN REINFORCEMENT BODIES, AND METHOD FOR PRODUCING THE CONNECTION BETWEEN THE COMPONENTS AND THE REINFORCEMENT BODIES |
Publications (2)
Publication Number | Publication Date |
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EP0184864A1 true EP0184864A1 (en) | 1986-06-18 |
EP0184864B1 EP0184864B1 (en) | 1990-10-03 |
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EP85201684A Expired - Lifetime EP0184864B1 (en) | 1984-12-05 | 1985-10-15 | Cast construction parts for internal-combustion engines incorporating reinforcing elements, and method for producing the connection between the parts and the elements |
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US (1) | US4739738A (en) |
EP (1) | EP0184864B1 (en) |
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FR2475534A1 (en) * | 1980-02-13 | 1981-08-14 | United Technologies Corp | COMPOSITE STRUCTURE HAVING CERAMIC MATERIAL REINFORCED WITH SILICON CARBIDE FIBERS |
GB2106433A (en) * | 1981-09-22 | 1983-04-13 | Ae Plc | Squeeze casting of pistons |
EP0078197A1 (en) * | 1981-10-20 | 1983-05-04 | Office National d'Etudes et de Recherches Aérospatiales (O.N.E.R.A.) | Mechanically and thermally resistant ceramic composite materials and their manufacture |
EP0107349A2 (en) * | 1982-09-24 | 1984-05-02 | Sumitomo Electric Industries Limited | Manufacturing method for fiber reinforced silicon ceramics sintered body |
EP0110064A1 (en) * | 1982-10-09 | 1984-06-13 | Toyota Jidosha Kabushiki Kaisha | Heat-resistant light alloy articles and method of manufacturing same |
EP0130105A1 (en) * | 1983-06-20 | 1985-01-02 | AEROSPATIALE Société Nationale Industrielle | Refractory fibre reinforced composite refractory material, and method of making the same |
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JPS54141209U (en) * | 1978-03-27 | 1979-10-01 | ||
US4245611A (en) * | 1978-09-05 | 1981-01-20 | General Motors Corporation | Ceramic insulated engine pistons |
JPS5815743A (en) * | 1981-07-22 | 1983-01-29 | Izumi Jidosha Kogyo Kk | Piston and its manufacture for internal-combustion engine |
DE3133209C2 (en) * | 1981-08-21 | 1985-04-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Hollow composite body, in particular body of revolution and method for its production |
DE3309699A1 (en) * | 1983-03-18 | 1984-09-27 | Feldmühle AG, 4000 Düsseldorf | HEAT-INSULATING LINING |
-
1984
- 1984-12-05 DE DE19843444406 patent/DE3444406A1/en not_active Withdrawn
-
1985
- 1985-10-15 EP EP85201684A patent/EP0184864B1/en not_active Expired - Lifetime
- 1985-10-15 DE DE8585201684T patent/DE3580005D1/en not_active Expired - Fee Related
- 1985-11-06 US US06/795,386 patent/US4739738A/en not_active Expired - Fee Related
- 1985-12-05 JP JP60274258A patent/JPS61135963A/en active Pending
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FR2475534A1 (en) * | 1980-02-13 | 1981-08-14 | United Technologies Corp | COMPOSITE STRUCTURE HAVING CERAMIC MATERIAL REINFORCED WITH SILICON CARBIDE FIBERS |
GB2106433A (en) * | 1981-09-22 | 1983-04-13 | Ae Plc | Squeeze casting of pistons |
EP0078197A1 (en) * | 1981-10-20 | 1983-05-04 | Office National d'Etudes et de Recherches Aérospatiales (O.N.E.R.A.) | Mechanically and thermally resistant ceramic composite materials and their manufacture |
EP0107349A2 (en) * | 1982-09-24 | 1984-05-02 | Sumitomo Electric Industries Limited | Manufacturing method for fiber reinforced silicon ceramics sintered body |
EP0110064A1 (en) * | 1982-10-09 | 1984-06-13 | Toyota Jidosha Kabushiki Kaisha | Heat-resistant light alloy articles and method of manufacturing same |
EP0130105A1 (en) * | 1983-06-20 | 1985-01-02 | AEROSPATIALE Société Nationale Industrielle | Refractory fibre reinforced composite refractory material, and method of making the same |
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EP0280480A2 (en) * | 1987-02-24 | 1988-08-31 | Carboride Corporation | Ceramic wall structures for engines and method of manufacture |
EP0280480A3 (en) * | 1987-02-24 | 1989-06-28 | Carboride Corporation | Ceramic wall structures for engines and method of manufacture |
Also Published As
Publication number | Publication date |
---|---|
EP0184864B1 (en) | 1990-10-03 |
US4739738A (en) | 1988-04-26 |
JPS61135963A (en) | 1986-06-23 |
DE3580005D1 (en) | 1990-11-08 |
DE3444406A1 (en) | 1986-06-05 |
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